N8554X
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
2ABC FLOOR PHOTOLUMINESCENCE STRIP IS CRACKED; DAMAGED AND HAS MOISTURE BUILD UP. REMOVED AND REPLACED FLOOR PHOTOLUMINESCENCE STRIP AT 2ABC IAW AMM 35-51-015.
3DEF FLOOR PHOTOLUMINESCENCE STRIP IS CRACKED, DAMAGED AND HAS MOISTURE BUILD UP. REMOVED AND REPLACED FLOOR PHOTOLUMINESCENCE STRIP AT 3DEF IAW AMM 33-51-15.
NUMBER 2 ENGINE FAILED ON TAKEOFF, REJECT AT APPROX 100 KIAS BRK ENERGY 21.1M FT-LB; INSPECTION REQUIRED ABOVE 30.0M FT-LM. DURING INITIAL EVALUTATION FAULT CODE 73-31552 IS PRESENT IN EEC REF FIM 73-31 TASK 803. PERFORMED GVI OF NR 2 ENGINE AND DISCOVERED HMU LEAKING FUEL. ACCOMPLISHED AN INSPECTION OF THE NR 2 ENGINE CHIP DETECTORS AND FOUND NO MAGNETIC PARTICLES IAW AMM 79-00-00. R & R FUEL PUMP IAW TASK CARD REF TTG8Q01BW3Y. R & R HMU IAW AMM 73-21-10. REQUIRES TEST 15 - 85% N1 LEAK CHECK PER POWERPLANT TEST REF TABLE 71-00-00. INSPECTED AND VERIFIED THE WORK PERFORMED ON CORRECTIVE ACTION NR 2, NO DEFECTS NOTED. REMOVED AND REPLACED NR 2 PUMP IAW TTG8Q01BW3Y ON MT 773-11-00; 85% LEAK CHECKED GOOD.
NUMBER 2 ENG FAILED ON TAKEOFF; REJECT AT APPROX 100 KIAS BRK ENERGY 21.1M FT-LB. INSPECTION REQUIRED ABOVE 30.0M FT-LM. DURING INITIAL EVALUTATION FAULT CODE 73-31552 IS PRESENT IN EEC IAW FIM 73-31, TASK 803. PERFORMED GVI OF NR 2 ENGINE AND DISCOVERED HMU LEAKING FUEL. ACCOMPLISHED AN INSPECTION OF THE NR 2 ENGINE CHIP DETECTORS AND FOUND NO MAGNETIC PARTICLES REF. AMM 79-00-00. R & R FUEL PUMP IAW TASK CARD REF TTG8Q01BW3Y. R & R HMU IAW AMM 73-21-10. REQUIRES TEST 15 - 85% N1 LEAK CHECK PER POWERPLANT TEST REF TABLE 71-00-00. INSPECTED AND VERIFIED THE WORK PERFORMED ON CORRECTIVE ACTION #2; NO DEFECTS NOTED. REMOVED AND REPLACED #2 PUMP REF TTG8Q01BW3Y ON MT 773-11-00; 85% LEAK CHECK GOOD
L1 DOOR SLIDE COVER 2EA CLIPS ARE LOOSE. RESECURED L1 DOOR SLIDE COVER 2EA CLIPS IAW SRM 51-40-02.
LEFT OTBD AFT FLASHLIGHT HAS RED LIGHT. R & R FLASHLIGHT ASSY IAW AMM 25-64-00 IN L/H AFT OTBD POSITION.
AFT MEGAPHONE INOPERATIVE. REMOVED AND REPLACED IAW AMM 25-64-00-SWA-804-NG-01.
AFT R/H F/A FLASHLIGHT NOT TESTING<[01] REPLACED AFT F/A FLASHLIGHT PER AMM 25-64-00.
EMERGENCY EXIT LIGHT LENS MISSING<[01] REPLACED MISSING CENTER AISLE CEILING EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01. OSD: 1/31/2025
PLASTIC PIECE FELL OFF DOOR R1 GIRT BAR.<[01] REPLACED R1 DOOR GIRT BAR EVAC RELEASE STOP PER AMM 25-66-00.
LEFT SIDE ROW 15CB OVER WING EXIT DOOR LIGHT INOPERATIVE<[01] OK TO CONT. PER MEL 33-2-04 SP#1 AUTH.#207613;[02] R&RD WINDOW LIGHT ASSEMBLY AT ROW 15CB IAW AMM 33-21-00; LOADED SOFTWARE AS REQUIRED AND OPS CHECK GOOD
1 AFT EMERGENCY FLASHLIGHT INOP<[01] REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY. OPS NORMAL. REF AMM 25-64-00
1 AFT EMERGENCY FLASHLIGHT INOP<[01] REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY. OPS NORMAL. REF AMM 25-64-00
RH SIDE SERVICE DOOR EMERGENCY LIGHT INOP<[01] R/R RH SLIDE SERVICE DOOR EMERGENCY LIGHT PER AMM 33-51-04
AFT CABIN F/OS SIDE FLASHLIGHT DOES NOT TEST<[01] SECURED AFT F/O FLASHLIGHT TO MOUNT PER SIP. NO DEFECTS NOTED.
OVERHEAD EMERGENCY EXIT SIGN MID CABIN CAME LOOSE<[01] RE-ATTACHED OVERHEAD EMERGENCY EXIT SIGN PLASTIC COVER REF 33-51-03
AFT CABIN FLASHLIGHT INOP<[01] R/R AFT CABIN FLASHLIGHT ASSY AND BATTERY IAW AMM 25-64-00 OPS CHECK GOOD
AFT CABIN FLASHLIGHT INOP<[01] R/R AFT CABIN FLASHLIGHT ASSY AND BATTERY IAW AMM 25-64-00 OPS CHECK GOOD
FWD ENTRY DOOR ESCAPE SLIDE; LOWER SKIRT MAKES HARD CONTACT WITH THE SCUFF PLATE WHEN OPENING AND CLOSING DOOR.<[01] ADJUSTED ESCAPE SLIDE ON FWD ENTRY DOOR PER AMM INTRODUCTION 2. STANDARD INDUSTRY PRACTICES STEP B AND AMM 25-66-01-400-801.;[02] VERIFIED CORRECTIVE ACTION ITEM AND MEASUREMENT FIELDS; CARD COMPLETE.
FWD LAV EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-802. OPS CHECK WAS GOOD.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.
#2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD IS CRACKED<[01] REMOVED AND REPLACED #2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD PER SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] R/H BS663 UPPER ATTACH ANGLE IS ON VAPOR BARRIER RBL8 WL167.68 REPAIRED BY REMOVED DAMAGE AREA; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 PAR 4 A-P.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
PANEL 221AF UPPER SURFACE HAS PULLED STRANDS OF FIBERGLASS<[01] UPPER SURFACE REPAIR ON PANEL 221AF COMPLETED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII INSPECTION REQUIREMENTS ARE MET.;[03] VERIFIED UPPER SURFACE REPAIR ON PANEL 221AF COMPLETED IAW SRM 53-00-50-2R-1
PANEL 241AF FORWARD RIGHT CORNER HAS EXPOSED CORE<[01] DUE TO EXTENT OF DAMAGE ON UPPER SURFACE OF PANEL FABRICATED NEW 241AF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1534398-1. INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A; INSERTS CURED USING HEAT LAMP AND THERMOMETER ATS2209 CAL DUE DATE 10/2024 THEN APPLIED TAPE AND PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 1A(NOTE); PARA 4A; TABLE 204; PARA 5S AND BOEING DWG 144A5910 ID:0127.;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION. JOB COMPLETE.;[03] VERIFIED MEASUREMENTS TABLE.
PANEL 221BF UPPER PLY IS DALAMINATED<[01] PANEL 221BF UPPER PLY DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS.
FLOOR SUPPORT CRACKED AT BS 380-400 LBL13 WL208.<[01] ALL STEPS COMPLETE REMOVED CRACKED FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE.<BR>LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-04 BOEING DWG 143A5400 INSTALLED NEW FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-02 BOEING DWG 143A5400 SHEET 184.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
FLOOR SUPPORT CRACKED AT BS 390 LBL51 WL208.<[01] REMOVED FLOOR SUPPORT ON BS 390 LBL 51 WL208 PER SRM 51-40-02 AND ENGINEER DWG: 143A5400 ID: 0183 (AND 0182).;[02] COMPLETED ALL STEPS REMOVED CRACKED FLOOR SUPPORT AT BS 390 LBL51 WL208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 390 LBL51 WL208. PER SRM 51-40-04 BOEING DWG 143A5400 ID: 0183 (AND 0182).INSTALLED NEW FLOOR SUPPORT AT BS 390 LBL51 WL208 PER SRM 51-40-02 ENGINEER DWG: 143A5400 ID: 0183 (AND 0182).;[03] REJECT: PIN PROTRUSION TO HEIGHT ON FLOOR SUPPORT AT BS 390 LBL51 WL208 <BR> SEE TTG8Q00PJG9K;[04] CORRECTED REJECTION IN ACTION 3. WORK PERFORMED AND DOCUMENTED ON CCN: TTG8Q00PJG9K.;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4.;[06] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.
FWD ENTRY DOOR MOPSILL CRACKED AT BS 303.9 LBL60 WL208<[01] INSTALLED FWD ENTRY DOOR MOPSILL IAW SRM 51-40-02-0G-0; BOEING DWG 140A9810 ID:71 REV:-; BOEING DWG 141A8110 ID:0022 REV:A AND BOEING DWG 141A8110 ID:0023 REV:-.;[02] CARD COMPLETE
WING CENTER SECTION - CRACKED SUPPORT FLOOR AT BS 540 LBL 2 WL 208 (MARKED)<[01] REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 540 BL0-LBL25 WL 208 PER SRM 51-40-02; DWG#143A0060.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
AFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREAS - CORROSION ON FLOOR BEAM BS 947 LBL 15.75 WL 208 (MARKED)<[01] FAULT RESOLVED ON OTHER FAULT<BR>DAMAGE TO BE REPAIRED ON FAULT TTG8Q00PEN6P DUE TO EXCEED LIMITS GIVEN PER SRM 53-70-51-1A-1 AND REQUIRED A REPAIR COVERING AREA REPORTED ON THIS CARD;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
AFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREAS - CORROSION ON FLOOR BEAM BS 947 LBL 23.5 WL 208 (MARKED)<[01] VERIFIED MEASUREMENT TABLE.;[02] REMOVED AND REPAIRED DAMAGES FLANGE OF THE FLOOR BEAM BS947 LBL9-LBL36 WL208 I.A.W SRM 53-70-51-2R-5 REPAIR 5 <BR>TASK COMPLETED;[03] VERIFIED CORRECTIVE ACTION #2
WING CENTER SECTION - CRACKED SUPPORT FLOOR AT BS 540 RBL 2 WL 208 (MARKED)<[01] REMOVED AND REPLACED FLOOR SUPPORT @ BS540 BL0-RBL25 WL208 PER SRM 51-40-02 AND DWG:143A0060 REV:A
CORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500I LBL21 TO RBL21<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CORROSION ON LOWER BULKHEAD SUPPORT WAS FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW CARGO BAY AFT NEW LOWER BULKHEAD SUPPORT AT BS 500I LBL 21 TO RBL 21 PER SRM 51-40-02-0G-0; DWG 143A7902 AND DWG 143A9481.;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.
CORROSION FWD CARGO BAY AFT SHIELD BS500+3 TO BS500+17 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] VERIFIED STEP 1;2 COMPLETE.;[02] DAMAGED SHIELD REPLACED DUE NO DATA FOUND ON SRM NEW SHIELD LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0; AND DWG 143A0080.;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.
RIGHT WING DEFLECTION CONTROL RIB WEB IS CRACKED AT THE O/B UPPER FASTENER CORNER (MARKED)<[01] UPDATED MEASUREMENTS; AND STEPS 1 & 2.;[02] REMOVED; REPLACED; AND INSTALLED A NEW R/W; T/E DEFLECTION CONTROL RIB WEB IAW SRM 51-40-02 AND BOEING DWG 115A2512. ALSO; UPDATED MEASUREMENTS AND VERIFIED.;[03] FINAL INSPECTION JOB COMPLETE.
CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS887 RBL11.5 WL168<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIED CORRECTION ACTION ITEM 1; AND MEASUREMENT TABLE.;[03] REMOVED ACB FLOOR SPLICE STRAP AT BS 887; LOCATED AND DRILLED NEW FLOOR SPLICE STRAP; AND INSTALLED NEW ACB FLOOR SPLICE STRAP AT BS 887; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 147A7500.;[04] VERIFIED CORRECTIVE ACTION #3<BR>VERIFIED MEASUREMENTS
CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727I+6 RBL10 WL156<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIED CORRECTION ACTION ITEM 1; AND MEASUREMENT TABLE.;[03] RECEIVED NEW AFT CARGO BAY FLOOR SPLICE STRAP BS727I+6 RBL10 WL156 ON PO # 945916 INSTALL WILL BE ON CARD # TTG8Q00NH2S8;[04] VERIFIED CORRECTIVE ACTIONS STEP 3.
CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL6 WL156<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIED CORRECTION ACTION ITEM 1; AND MEASUREMENT TABLE.;[03] RECEIVED NEW AFT CARGO BAY FLOOR SPLICE STRAP BS727D+6 RBL6 WL156 ON PO # 945916 INSTALL WILL BE ON CARD # TTG8Q00NH2SA;[04] VERIFIED CORRECTIVE ACTIONS STEP 3.
CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11 WL156<[01] UPDATED MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIED CORRECTION ACTION ITEM 1; AND MEASUREMENT TABLE.;[03] RECEIVED NEW AFT CARGO BAY FLOOR SPLICE STRAP BS767+6 RBL11 WL156 ON PO # 867103 INSTALL WILL BE ON CARD # TTG8Q00NH2S6;[04] ADDED PARTS;[05] VERIFIED CORRECTIVE ACTIONS STEP 3 AND MEASUREMENTS TABLE.
CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727G+19' TO BS787+1' LBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] VERIFIED STEPS 1-6;[03] MADE CORRECTIONS AND CHANGED STEP STATUS TO PARTIAL ON STEPS 4 AND 6;[04] CERTIFIED;[05] EVALUATED CORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT BS 727G+19 TO 787+1; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED DAMAGED SECTION FROM BS727G+10 TO 787+8; FABRICATED REPAIR PARTS; DRILLED; LOCATED; APPLIED CHEMICAL CONVERSION COATING; PRIMED ASSEMBLED; AND INSTALLED; ALL IAW SRM51-40-02-0G-0; SRM 51-40-05-0G-0;SRM 53-00-53-2R=5; SRM 51-20-01-0G-0; DWG 146A7500; AMM 51-21-72-370-804.;[06] VERIFIED CORRECTIVE ACTION 5
CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727E+19' TO BS767 RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] VERIFIED STEPS 1-6;[03] MADE CORRECTIONS AND CHANGED STEP STATUS TO PARTIAL ON STEPS 4 AND 6;[04] CERTIFIED;[05] CORROSION DAMAGE ON ACB R/H FLOOR TO SIDEWALL SUPPORT BS727E+19 TO BS767; RBL22; WL156 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. CUT AND REMOVED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT BS727+12 TO BS767; RBL22; WL156 PER SRM 53-00-53-2R-5. LOCATED; DRILLED AND INSTALLED REPLACEMENT FLOOR TO ACB R/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS COMPLETE PER SRM 53-00-53-2R-5.;[06] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 5 AND MEASUREMENT TABLE.
CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS787+18' TO BS827+10' RBL 26 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB WAS FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW AFT CARGO BAY SUB THRESHOLD WEB PER SRM 51-40-02-0G-0; DWG 146A8340 AND DWG 146A8120.;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.
CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] CORROSION ON SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED AS PER SRM 51-10-02. REMOVED OLD SHIELD. LOCATED; DRILLED AND INSTALLED REPLACEMENT SHIELD FWD OF CARGO DOOR BS767-794; RBL22; WL156 PER DWG 146A0081; SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION 2.<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETED.
CORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE.;[03] CORROSION ON FLOOR TO SIDEWALL SUPPORT WAS FOUND TO BE OUT OF LIMITS; REMOVE AND REPLACED SIDEWALL SUPPORT AT BS 500A TO 500I RBL 22 WL 156 PER SRM 51-40-02-0G-0 AND DWG 143A7500.;[04] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 3 AND MEASUREMENT TABLE.
CORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS440+10' TO BS490' RBL 26.5 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] REMOVED AND REPLACED FWD CARGO BAY SUB THRESHOLD WEB BS 440-492 RBL 26.5 WL 156 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 143A8330.;[03] UPDATED PART USAGE
PANEL 194CL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL WITH OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE. JOB COMPLETE.
FLAP MALFUNCTION AT FLAPS 5. NO ASYMMETRY NOTED. T/EDGE FLAPS DISAGREE QRH RUN. C/W ALTN FLAPS DUTY CYCLE<[01] REMOVED AND REPLACED T/E FLAP POSITION INDICATOR PER M/M OPS CHECKED GOOD PER M/M 27-58-02; ALSO R AND R FSEU BOX PER M/M 27-58-02 OPS CHECKED GOOD- ALSO SERVICED ALL FLAPS TRANSMISSIONS PER M/M 27-51-51
FLAP MALFUNCTION AT FLAPS 5. NO ASYMMETRY NOTED. T/EDGE FLAPS DISAGREE QRH RUN. C/W ALTN FLAPS DUTY CYCLE<[01] REMOVED AND REPLACED T/E FLAP POSITION INDICATOR PER M/M OPS CHECKED GOOD PER M/M 27-58-02; ALSO R AND R FSEU BOX PER M/M 27-58-02 OPS CHECKED GOOD- ALSO SERVICED ALL FLAPS TRANSMISSIONS PER M/M 27-51-51
FWD SVC DOOR SLIDE GIRYT BAR HARD TO INSTALL/REMOVE<[01] REPOSITION FWD SVC DOOR ESCAPE SLIDE IN CONTAINER PER AMM 25-66-01
MID CABIN OVERHEAD EXIT LIGHT FWD LENS MISSING<[01] INSTALLED NEW LENS PER AMM 3-51-01
FWD FACEPLATE OF CENTER AISLE EXIT LIGHT FELL OFF. / [01] RE-INSTALLED FWD LENS COVER ON CTR AISLE EXIT LIGHT PER AMM 33-51-01.
EXTERNAL GROUND POWER RECEPTACLE SURROUND DOUBLER TAB HAS A CRACK WITH MISSING MATERIAL AT LOWER LOBE ACROSS TWO FASTENERS IN ZONE 2. BETWEEN STA 224.8 AND 235.8 6.5' ABOVE 23R / [01] INSTALLED PERMANENT REPAIR PER SRM 53-10-15-2R-4-B00449 (REPAIR 4 )
R1 FORWARD GALLEY SERVICE DOOR BINDS WHEN OPENING FROM INSIDE OF AIRCRAFT ; / [01] LUBED R1 FORWARD GALLEY SERVICE DOOR AND PERFORMED FWD GALLEY SERVICE DOOR TEST IN REFERENCE TO AMM 52 - 41 - 00 OPS CHECK IS OK
AFT LEFT EMERGENCY FLASHLIGHT NOT CHARGING ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) REF LOG PAGE 1903931 / REPLACED AFT EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00 OPS CK GOOD CL # 92945
R2 DOOR SLIDE GIRT HANGING TOO LOW. REPOSITIONED R2 DOOR SLIDE GIRT, PER AMM 25-66-01 AMT 44445 INSP 52251.
L1 DOOR LOWER EMERGENCY EXIT SIGN LIGHT LENS BROKEN. R&R LENS PER AMM.